NTSB CAROL · Event
Event CHI90LA259
Registry · N2229B
FAA Aircraft Registry record.
Make / Model
LUSCOMBE 8A
Year of manufacture
1949 · 41 years old at event
Engine
CONT MOTOR C90 SERIES (95 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19550930
ADS-B equipped
Yes — Mode-S A1EC04
Registrant of record
B & G FLYING SERVICE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the loss of engine power for undetermined reasons while executing a go-around with insufficient runway remaining for a forced landing. A factor in the accident was the structures at the end of the runway that the pilot was attempting to avoid. This report was modified on February 9, 2005.
Factual narrative
On September 6, 1990, at 1845 CDT, a Luscombe 8A, N2229B, operated by an airline transport pilot, was substantially damaged when it nosed over during landing roll following an emergency landing at Lebert Flying L Airport, Lebanon, Illinois. The pilot was not injured. The personal flight was conducted under 14 CFR Part 91 and no flight plan was filed. The local flight originated at Lebert Flying L Airport at 1815 CDT. Visual meteorological conditions prevailed at the time of the accident. A witness who observed the airplane's approach stated that the approach was "hot and high." The pilot stated that he was too high and fast at the landing threshold, that he applied power to execute a go-around, but the engine "popped and quit." He stated that he cycled the carburetor heat to the off position after the engine quit, and also cycled the mixture control during his unsuccessful attempt to restart the engine at low altitude. He stated that when the engine failed to restart he concentrated on landing on the remaining runway. He landed the airplane near the departure end of the runway and applied maximum braking to avoid cement company structures off the end of the runway and the airplane nosed over. The investigation determined that the carburetor heat control was jammed in the off position and that the carburetor was dislodged from its base. The temperature at the time of the accident was 97° F, and the dew point was 72°. This report was modified on February 9, 2005. The pilot was landing at a private grass strip. Witnesses described the approach as hot and high. The engine lost power when the pilot attempted to execute a go-around. The pilot landed long, applied maximum braking to avoid structures at the end of the runway, and the airplane nosed over. The investigation indicated that the carburetor heat control was jammed in the off position. The pilot stated that he pulled the carburetor heat control to the off position to cycle it, along with the mixture, during his unsuccessful attempt to restart the engine. He stated that he left the carburetor heat control in the off position to concentrate on the forced landing from a low altitude. The airplane was placarded with a caution that carburetor heat was required for takeoffs and landings. There was a slight risk of light carburetor icing based on temperature and dew point values. However, with the high atmospheric temperature (97 degrees), a sudden, maximum temperature drop of 60 degrees would have resulted in a carburetor temperature above freezing (37 degrees). This report was modified on February 9, 2005. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_CHI90LA259.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2020 · Conference paper
Concurrent Sessions: Session 8A - Technology in Aviation
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
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